GB1193136A - A Structural Element adapted to be Liquid Cooled - Google Patents

A Structural Element adapted to be Liquid Cooled

Info

Publication number
GB1193136A
GB1193136A GB54410/67A GB5441067A GB1193136A GB 1193136 A GB1193136 A GB 1193136A GB 54410/67 A GB54410/67 A GB 54410/67A GB 5441067 A GB5441067 A GB 5441067A GB 1193136 A GB1193136 A GB 1193136A
Authority
GB
United Kingdom
Prior art keywords
tubes
components
liquid cooled
making
applied layer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB54410/67A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bolkow GmbH
Original Assignee
Bolkow GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bolkow GmbH filed Critical Bolkow GmbH
Publication of GB1193136A publication Critical patent/GB1193136A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
GB54410/67A 1966-12-15 1967-11-29 A Structural Element adapted to be Liquid Cooled Expired GB1193136A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEB90325A DE1264160B (de) 1966-12-15 1966-12-15 Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
US68317667A 1967-11-15 1967-11-15

Publications (1)

Publication Number Publication Date
GB1193136A true GB1193136A (en) 1970-05-28

Family

ID=25968260

Family Applications (1)

Application Number Title Priority Date Filing Date
GB54410/67A Expired GB1193136A (en) 1966-12-15 1967-11-29 A Structural Element adapted to be Liquid Cooled

Country Status (4)

Country Link
US (1) US3690103A (enrdf_load_stackoverflow)
DE (1) DE1264160B (enrdf_load_stackoverflow)
FR (1) FR1567108A (enrdf_load_stackoverflow)
GB (1) GB1193136A (enrdf_load_stackoverflow)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4336124A (en) 1979-07-16 1982-06-22 Compagnie Generale Des Etablissements Michelin Electrodes with current outlets
RU2325545C1 (ru) * 2006-11-07 2008-05-27 Федеральное государственное унитарное предприятие "Воронежский механический завод" Внутренняя оболочка сопла камеры жидкостного ракетного двигателя

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1941297B2 (de) * 1969-08-14 1971-11-18 Regenerativ gekuehlte brennkammer und oder schubduese
DE1941296B2 (de) * 1969-08-14 1971-09-30 Messerschmitt Bolkow Blohm GmbH, 8000 München Durch ein fluessiges medium regenerativ gekuehlte brenn kammer mit schubduese
DE2137109C3 (de) * 1971-07-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Herstellung einer regenerativ gekühlten Raketenbrennkammer
US3784152A (en) * 1972-04-24 1974-01-08 Ici Ltd Process of producing a composite mold having cooling pipes embedded therein
US3782118A (en) * 1972-12-18 1974-01-01 Messerschmitt Boelkow Blohm Regeneratively cooled thrust gas generator construction and method of making same
DE2657474A1 (de) * 1976-12-18 1978-06-22 Messerschmitt Boelkow Blohm Verfahren zum herstellen von regenerativ gekuehlten raketenbrennkammern und/oder schubduesen
DE3004033C2 (de) * 1980-02-05 1986-04-10 Klöckner-Humboldt-Deutz AG, 5000 Köln Wärmegeschützte Kraftstoffeinspritzdüse für Brennkraftmaschinen und Verfahren zur Herstellung einer solchen Einspritzdüse
US4586226A (en) * 1983-09-30 1986-05-06 Rockwell International Corporation Method for fabricating a small-orifice fuel injector
US4707225A (en) * 1986-01-06 1987-11-17 Rockwell International Corporation Fluid-cooled channel construction
US4786015A (en) * 1986-12-31 1988-11-22 Sundstrand Corporation Structural cooling unit
EP0374382A1 (de) * 1988-12-21 1990-06-27 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Kühlung von Hyperschallantriebskomponenten
US4942653A (en) * 1989-08-25 1990-07-24 Rockwell International Corporation Production method for a channeled wall thrust nozzle
DE4015204C1 (enrdf_load_stackoverflow) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
DE4115403A1 (de) * 1991-05-10 1992-11-12 Mtu Muenchen Gmbh Duesenwand
US5467528A (en) * 1991-12-23 1995-11-21 United Technologies Corporation Method of making a tubular thermal structure
US5371945A (en) * 1991-12-23 1994-12-13 United Technologies Corporation Method of making a tubular combustion chamber construction
US5386628A (en) * 1991-12-23 1995-02-07 United Technologies Corporation Method of making a diffusion bonded rocket chamber
US5375325A (en) * 1992-05-26 1994-12-27 United Technologies Corporation Method of making a rocket chamber construction
DE4321393C2 (de) * 1993-06-26 1996-08-22 Daimler Benz Aerospace Ag Wandstruktur, insbesondere für ein Staustrahltriebwerk
US5557928A (en) * 1994-08-16 1996-09-24 United Technologies Corporation Tube rocket thrust chamber construction and method
FR2776215B1 (fr) 1998-03-20 2000-06-16 Snecma Procede de fabrication d'un circuit regeneratif a fort flux thermique, notamment pour chambre de combustion de moteur-fusee
US6131280A (en) * 1998-11-30 2000-10-17 United Technologies Corporation Method of repairing a rocket thrust chamber
DE19901422C2 (de) * 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk
DE19915082C1 (de) * 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
US6582542B1 (en) * 1999-07-07 2003-06-24 Mark C. Russell Method of producing a channeled wall fluid control apparatus
DE10043303B4 (de) * 2000-09-02 2004-06-09 Astrium Gmbh Raketentriebwerk in Segmentbauweise
WO2002055862A1 (en) * 2001-01-11 2002-07-18 Volvo Aero Corporation Rocket engine member and method for manufacturing a rocket engine member
ATE393875T1 (de) * 2001-01-11 2008-05-15 Volvo Aero Corp Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds
FR2838183B1 (fr) * 2002-04-09 2004-07-09 Snecma Propulsion Solide Structure d'echangeur thermique haute temperature
AU2003238988A1 (en) * 2002-05-28 2003-12-12 Volvo Aero Corporation Wall structure
US6883220B2 (en) * 2002-07-17 2005-04-26 The Boeing Company Method for forming a tube-walled article
US7464537B2 (en) * 2005-04-04 2008-12-16 United Technologies Corporation Heat transfer enhancement features for a tubular wall combustion chamber
DE102008011502A1 (de) 2008-02-25 2009-09-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung
US20100313589A1 (en) * 2009-06-13 2010-12-16 Brent Alden Junge Tubular element
RU2516723C2 (ru) * 2012-02-03 2014-05-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ изготовления тракта регенеративного охлаждения камеры жидкостного ракетного двитателя
DE102017129321B4 (de) 2017-12-08 2024-11-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammervorrichtung, Fahrzeug
KR102468746B1 (ko) * 2020-11-18 2022-11-18 한국항공우주연구원 열교환 구조를 포함하는 연소기 및 이를 포함하는 로켓
CN113389657B (zh) * 2021-07-27 2022-09-30 中国人民解放军国防科技大学 一种高温流体通道

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE611581C (de) * 1933-08-05 1935-04-01 Elmore S Metall Aktien Ges Galvanoplastische Herstellung von Platten oder Behaeltern aus Metallen
DE716175C (de) * 1935-02-09 1942-01-14 Eugen Saenger Dr Ing Raketenmotor
US2958183A (en) * 1949-02-24 1960-11-01 Singelmann Dietrich Rocket combustion chamber
US3190070A (en) * 1950-04-05 1965-06-22 Thiokol Chemical Corp Reaction motor construction
US2844939A (en) * 1954-10-04 1958-07-29 Gen Electric Tube-bundle combustion chamber
GB843923A (en) * 1957-01-17 1960-08-10 Havilland Engine Co Ltd Apparatus in which heat exchange takes place between fluids
US3022230A (en) * 1959-06-16 1962-02-20 Camin Lab Inc Process for electroforming grooved and channeled bodies
US3349464A (en) * 1962-06-29 1967-10-31 Aerojet General Co Method of making rocket combustion chamber
US3254487A (en) * 1963-01-04 1966-06-07 Edward F Baehr Rocket motor casing

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4336124A (en) 1979-07-16 1982-06-22 Compagnie Generale Des Etablissements Michelin Electrodes with current outlets
US4421609A (en) 1979-07-16 1983-12-20 Compagnie Generale Des Etablissements Michelin Process for producing electrode with current outlets
RU2325545C1 (ru) * 2006-11-07 2008-05-27 Федеральное государственное унитарное предприятие "Воронежский механический завод" Внутренняя оболочка сопла камеры жидкостного ракетного двигателя

Also Published As

Publication number Publication date
DE1264160B (de) 1968-03-21
US3690103A (en) 1972-09-12
FR1567108A (enrdf_load_stackoverflow) 1969-05-16

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee